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Airworthiness Directives; Airbus Model A320-111 Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2005-10-12 · Effective 2005-10-27 · 70 FR 59229

Document

Document number
05-20069
Federal Register citation
70 FR 59229
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Airbus Model A320-111
Publication date
2005-10-12
Effective date
2005-10-27
FAA docket
Docket No. FAA-2005-22626

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A320-111 airplanes. The existing AD currently requires repetitive inspections for cracking in the front and rear faces and at the crown fittings of the upper stringers of the center wing box and applicable repairs. This new AD requires continuing the repetitive inspections at revised thresholds and intervals, and applicable repairs. This AD results from a manufacturer survey of airplanes affected by the existing inspection program that led to the consequent revision of the thresholds and intervals of the repetitive inspections. We are issuing this AD to detect and correct fatigue cracking of the upper stringers of the center wing box, which could lead to loss of structural integrity of the wing.

Source

Authoritative
Federal Register document
Machine
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